On-Line Trajectory Generation Method Based on Closed-Form Analytical Solution for Reusable Launch Vehicle.

Autor: LI Zhao-ying1 lizhaoying@buaa.edu.cn, HUANG Xing-li2, LI Hui-feng1
Zdroj: Journal of Astronautics / Yuhang Xuebao. Jun2013, Vol. 34 Issue 6, p755-762. 8p.
Databáze: Academic Search Ultimate